Department of Aerospace Engineering, College of Science and Technology, Nihon University
Department of Aerospace Engineering, College of Science and Technology, Nihon University
Department of Aerospace Engineering, College of Science and Technology, Nihon University
Department of Aerospace Engineering, College of Science and Technology, Nihon University
Department of Aerospace Engineering, College of Science and Technology, Nihon University
Hosoya Pyro-Engineering
Hosoya Pyro-Engineering
Division for Space Propulsion and Propellants, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
出版者
宇宙航空研究開発機構
出版者（英）
Japan Aerospace Exploration Agency (JAXA)
雑誌名
宇宙航空研究開発機構研究開発報告: 高エネルギー物質研究会: 平成23年度研究成果研究成果報告書
雑誌名(英)
JAXA Research and Development Report: Collaborative Research Activity on Energetic Materials Research Report FY2011
In this research we obtained ignition delay time, chemical ignition delay time, and activation energy of the Ammonium dinitramide (ADN) / Ammonium nitrate (AN) composite propellants. In the results ignition delay time and chemical ignition delay time decrease with increasing atmosphere temperature and increasing concentration of ADN. Activation energy of ADN/AN composite propellant decrease at concentration of ADN between 40 [mass%] and 60 [mass%]. It is consider that reaction of ADN/AN propellant is changed by increasing concentration of AN.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
ADN/AN系コンポジット推進薬の着火特性
65204003.pdf
(705.26KB)
